Item Details

Effect of Speed Brakes on the Supersonic Aerodynamic Characteristics of a Variable-Sweep Tactical Fighter Model at Mach Numbers From 1.60 to 2.50

by Celia S. Richardson
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, 1968.
Language
English
Series
NASA Technical Note
Description
33 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • "N68-33669."
  • Includes bibliographical references (p. 9-10).
Series Statement
NASA technical note ; NASA TN D-4773
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Effect of speed brakes on the supersonic aerodynamic characteristics of a variable-sweep tactical fighter model at Mach numbers from 1.60 to 2.50 / c| by Celia S. Richardson.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, c| 1968.
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    a| 33 p. : b| ill. ; c| 28 cm.
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    a| NASA technical note ; v| NASA TN D-4773
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    a| Prepared at Langley Research Center.
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    a| Includes bibliographical references (p. 9-10).
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    a| Mode of access: Internet.
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    a| Airplanes x| Brakes.
    650
      
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    a| Mach number.
    650
      
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    a| Fighter planes.
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    0
    a| Aerodynamics, Supersonic.
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    a| Langley Research Center.
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